Repair EGI 764+429+JAIC

ATTACHMENT 2 - STATEMENT OF WORK (SOW) 70Z03826QJ0000095 Page 1 of 5 1.0 Contractor Requirements 1.1 The United States Coast Guard (USCG) will furnish the components and quantities specified in the following table for repair: Description Quantity National Stock Number (NSN) Part Number (P/N) EGI+764+429+JAIC 8 1680-01-HS1-9691 HG9869K1-001 1.2 The components are utilized on the MH-60T aircraft. Upon receipt of the components, the Contractor shall perform a teardown, test and evaluation to determine the condition of the component. If the component is found to be Ready for Issue (RFI) a firm-fixed price test and evaluation fee would be applicable. Any components determined to be Beyond Economical Repair (BER); the Contractor will be allowed a firm-fixed BER/Scrap fee would be applicable. Only one of the firm-fixed prices below would be applicable: Service Total Test/Evaluation TBD at time of service BER/Scrap Fee TBD at time of award 1.2.1 When a component is found to be BER, the Contractor shall prepare a failure data report in accordance with (IAW) Section 2.11. This report shall be included with the returned component. The Contracting Officer will provide disposition instructions IAW Section 2.9 via a modification for all components found to be BER. 2.0 Repair 2.1 Non-RFI components shall be repaired and returned to RFI condition in accordance with (IAW) the original equipment manufacturer (OEM) functional performance specifications. Components shall be repaired for the specific fault noted on the DD Form 1577-2, Unserviceable (Repairable) Tag-Material, or CG-1577-A (11-90), Unsatisfactory Report Tag, which will be attached to each non-RFI component. The Contractor shall perform an inspection and correct all deficiencies found. This shall include, but is not limited to, replacement of missing or broken parts and the removal of any foreign matter or corrosion. 2.2 During inspection and functional test, the presence of corrosion in a component shall constitute reason for a more thorough disassembly and inspection. Should corrosion be found, disassembly shall be made to the extent necessary to remove corrosion or replace the part, or parts, affected. Corroded parts shall be replaced, except in those cases where removal of corrosion from a part will not impair efficiency or safe operation of the part. Corrosion removal and treatment of affected areas will be accomplished IAW OEM specifications and Federal Aviation Administration (FAA) Advisory Circular AC 43-4B, dated 9/11/2018, Corrosion Control for Aircraft. 2.3 Work under this purchase order shall be performed at the Contractor’s facility or USCG approved facility. The Contractor shall provide all necessary parts, materials, labor, tooling, test equipment and facilities to evaluate and repair the components listed in this purchase order at the firm-fixed prices listed in the schedule (or modification). 2.4 Repair services must be performed IAW the procedures established in this SOW. The documents are listed in order of precedence. Latest revisions of any instruction or manual shall apply. The information contained within is not intended to be all inclusive nor to detract from or modify procedures -- 1 of 5 -- ATTACHMENT 2 - STATEMENT OF WORK (SOW) 70Z03826QJ0000095 Page 2 of 5 outlined in the manuals. If the applicable technical manual does not cover a procedure, the Contractor shall utilize the OEM repair manual. If the OEM manual does not cover a procedure, the Contractor shall utilize the best commercial business practice. Where an application of “best commercial practice” is in conflict with these manuals, the Contracting Officer may approve deviation from requirements. When applicable, each manual will specify if the Export Control Act applies. The following documents are required to complete the services required by this acquisition. The USCG does not own, nor can it provide the technical documents specified herein. • All OEM shop, inspection, overhaul, repair, or other OEM Component Maintenance Manuals (CMM) • All OEM service bulletins, amendments, modifications, and specifications as applicable 2.5 The Contractor shall have access to required repair specifications and test/acceptance criteria and data to ensure all components are tested and repaired IAW the current specifications and procedures. The USCG may review repair manuals and performance/test/ acceptance criteria as required. The Contractor is solely responsible for obtaining all specifications required for this effort. Original design or functional capabilities of the end component and parts thereof shall not be changed unless authorized or directed by the requirements of this SOW. 2.6 Parts of a component found to be in a serviceable condition as a result of functional testing shall be reused. Missing parts and parts found to be defective or that require replacement by manufacturer’s instructions shall be replaced with parts meeting the manufacturer’s specifications and drawings or as otherwise authorized in writing by the Contracting Officer. Replacement parts shall be new and accompanied with OEM traceability. The cost for parts that are replaced systematically during repair shall be included in the price listed in the schedule for these operations. 2.7 Prices do not include components that have been cannibalized or severely damaged due to mishandling. Additionally, USCG aircraft is used primarily around salt water at low altitude for search and rescue missions. Therefore, corrosion is to be anticipated and is considered "normal" for the aircraft. Corrosion does not constitute unusual damage. 2.8 Components received which indicate obvious misuse, cannibalization, or severe damage due to mishandling or crash damage may dictate an exclusion from the prices specified in the contract schedule. Such components shall be inspected, repair costs determined, and authorization to proceed obtained from the Contracting Officer prior to commencement of work. Once notified of a p…